FTW96LA275
1996-06-24 · LAS ANIMAS, Colorado, United States · None · 1 aircraft · Status: Completed
Airport 7V9
Aircraft involved
Probable cause & findings
inadequate preflight planning/preparation by the pilot. Factors relating to the accident were: the unfavorable wind condition for takeoff, and the terrain condition beyond the end of the runway.
Factual narrative
On June 24, 1996, at 1130 mountain daylight time, a Rockwell S2R, N4907X, exited the end of the runway during the takeoff roll at Las Animas County Airport, Las Animas, Colorado. The commercial pilot was not injured and the aircraft sustained substantial damage. The flight was a local area aerial application flight operating under Title 14 CFR Part 137. Visual meteorological conditions prevailed and no flight plan was filed. According to the pilot, he was taking off from runway 26 and did not clear a ditch located at the end of the runway. Density altitude at the time was 6,500 feet and the wind was reported by the pilot to be from 010 degrees magnetic at 10 miles per hour. The pilot said that airspeed was not building at a "continuous rate" and he had insufficient runway available to abort the takeoff. He said he dumped the load (24D herbicide) and the aircraft exited the end of the runway up an inclined ditch bank which "launched" the aircraft into the air. The aircraft stalled left wing down and impacted the ground in a nose down 15 degree left bank. During the takeoff roll on runway 26, the aircraft did not attain sufficient airspeed to achieve flight. The pilot reported that the airplane did not accelerate at a continuous rate, and there was insufficient runway remaining to abort the takeoff. He dumped the load, but the aircraft overran the end of the runway and went up an incline bank, which launched it into the air. A stall ensued and the aircraft impacted the ground in a nose down 15 degree left wing down attitude. Wind at the time was from 010 degrees at 10 miles per hour. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_FTW96LA275.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- NASA NTRS 2026 · Conference Paper Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER) Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…